Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
Patents for F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699)
01/2011
01/05/2011EP2270312A1 Aero- or hydrodynamic construction
01/05/2011EP2268910A2 Bypass turbojet engine nacelle
01/05/2011CN101939528A Variable area fan nozzle with bypass flow
01/05/2011CN101936543A Jet combustion chamber with electric propulsion
01/05/2011CN101936238A Jet engine with electric propulsion function
01/05/2011CN101634257B Secondary-duct combination spray pipe of engine
01/04/2011CA2646629C Integrated engine exhaust systems and methods for drag and thermal stress reduction
01/04/2011CA2618661C Infrared suppression system
01/04/2011CA2460549C Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine
12/2010
12/29/2010EP2126321B1 Gas turbine comprising a guide ring and a mixer
12/29/2010EP2066895B1 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle
12/28/2010US7857093 Engine inlet deep acoustic liner section
12/22/2010CN101922380A Actuation system for a translating variable area fan nozzle
12/22/2010CN101922379A Translating variable area fan nozzle providing an upstream bypass flow exit
12/21/2010US7854124 Combined control for supplying cooling air and support air in a turbine engine nozzle
12/21/2010US7854123 Turbomachine nozzle cover provided with triangular patterns having pairs of vertices for reducing jet noise
12/16/2010WO2010144181A1 Gas turbine engine assembly and corresponding operating method
12/16/2010WO2010142881A1 Thrust reversing device
12/16/2010US20100314194 Trailing edge for an aircraft engine, of the type with moving chevrons
12/16/2010CA2764437A1 Thrust reversing device
12/15/2010EP2069631B1 Fan variable area nozzle positional measurement system
12/15/2010EP2066890B1 Modulating flow through gas turbine engine cooling system
12/14/2010US7849695 Rocket thruster comprising load-balanced pintle valve
12/14/2010US7849670 Propulsion system with integrated rocket accelerator
12/09/2010WO2010139877A1 Thrust reverser for a dual-flow turbine engine nacelle
12/09/2010US20100307163 Fiber-based ablative and high temperature pre-preg material
12/09/2010US20100307130 Non-handed thrust reverser for installation on handed aircraft gas turbine propulsion engines
12/09/2010CA2763523A1 Thrust reverser for a dual-flow turbine engine nacelle
12/08/2010EP2258926A2 Control mechanism
12/08/2010EP2257704A2 Device for reducing the noise generated by an aircraft jet engine with fluid jets of the same orientation
12/08/2010CN101910598A Door-type thrust reverser for a jet engine
12/08/2010CN101909997A Twelve-hour structure for thrust reverser, in particular with grids
12/07/2010US7845176 Mode strut and divergent flap interface
12/07/2010US7845175 Heat shield for mounting on a heat-radiating object, particularly on a rocket engine
12/07/2010US7845156 Turbofan exhaust system
12/02/2010WO2010136545A1 Turbine engine comprising an exhaust-gas guide cone with a sound suppressor
12/02/2010WO2010136369A1 Aircraft engine nacelle comprising a mobile cowl moved by electric motors
12/02/2010CA2761761A1 Aircraft engine nacelle comprising a mobile cowl moved by electric motors
12/02/2010CA2761601A1 Turbine engine comprising an exhaust-gas guide cone with a sound suppressor
12/01/2010EP2256327A1 Noise reducing device, and jet propulsion system
12/01/2010EP2255086A1 Stave and ring cmc nozzle
12/01/2010CN101898638A Anticollision technology for JF-17 thunder spout
11/2010
11/30/2010CA2538899C Passive exhaust suppressor and method
11/25/2010WO2010133780A1 Cowling for a turbine engine nozzle provided with side fins for reducing the noise of the jet
11/25/2010CA2761510A1 Cowling for a turbine engine nozzle provided with side fins for reducing the noise of the jet
11/24/2010EP2252512A2 Device for reducing turboprop infrared emissions
11/24/2010CN101896712A Nacelle for aircraft engine having a nozzle with a variable section
11/23/2010US7836701 Infrared suppression system
11/23/2010US7836700 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws
11/23/2010US7836681 Mechanism for a vectoring exhaust nozzle
11/23/2010CA2460742C Device for controlling propulsive flow mixture for aircraft reactor
11/11/2010US20100281874 Airflow vectoring member
11/10/2010EP1680589B1 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
11/09/2010US7827802 Variable-section flow mixer for a double-flow turbojet for a supersonic airplane
11/09/2010CA2486172C Variable area thrust reverser nozzle
11/09/2010CA2435559C Tubular sound attenuation part for the engine air intake of an aircraft
11/03/2010EP2245290A1 System for controlling a plurality of functions of a turbojet engine
11/03/2010EP2245289A1 Trailing edge for an aircraft engine, of the type with moving chevrons
11/03/2010EP2109712B1 Aircraft nacelle incorporating a thrust-reversing device
11/03/2010CN101576025B Multi-mode spraying pipe with adjustable throat for ramjet engine
11/02/2010US7823836 Optimal sun safe attitude for satellite ground tracking
10/2010
10/30/2010CA2701405A1 Structural reinforcement strut for gas turbine case
10/28/2010WO2010122253A1 Torque limiter in particular for an actuator of the nacelle of an aircraft turbojet engine
10/28/2010WO2009133272A8 Device for reducing the noise generated by an aircraft jet engine with fluid jets of the same orientation
10/28/2010WO2009133271A8 Device for reducing noise generated by an aircraft jet engine with curve ducts
10/28/2010US20100270428 Thrust reverser assembly with shaped drag links
10/28/2010US20100269512 Gas turbine engine having slim-line nacelle
10/28/2010US20100269511 Nacelle for aircraft engine having a nozzle with a variable section
10/28/2010US20100269486 Gas turbine engine having slim-line nacelle
10/28/2010US20100269485 Integrated variable area nozzle and thrust reversing mechanism
10/28/2010CA2758646A1 Torque limiter in particular for an actuator of the nacelle of an aircraft turbojet engine
10/27/2010EP2243946A2 Actuators system
10/27/2010EP2243945A2 Thrust reverser assembly with shaped drag links
10/27/2010EP2242922A1 System for controlling the cowl of a turbojet engine nacelle thrust reverser
10/27/2010EP2242921A2 Control system for turbojet engine nacelle
10/26/2010US7819224 Assembly for reducing noise in turbofan engines
10/26/2010CA2418357C Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
10/21/2010WO2010119210A1 Actuator system for a mobile panel of a nacelle of a turbojet
10/21/2010WO2010119209A1 Control system for a turboreactor nacelle
10/21/2010WO2010119204A1 Thrust reversal device
10/21/2010CA2758134A1 Actuator system for a mobile panel of a nacelle of a turbojet
10/21/2010CA2758132A1 Control system for a turboreactor nacelle
10/21/2010CA2758091A1 Thrust reversal device
10/20/2010EP2240317A2 Thermally conductive structure
10/20/2010CN201610800U 一种可调后涵道引射器 After an adjustable ducted ejector
10/20/2010CN201610799U 一种可调前涵道引射器 An adjustable front ducted ejector
10/19/2010CA2472605C Turbofan variable fan nozzle
10/19/2010CA2418879C Methods and apparatus for varying gas turbine engine inlet air flow
10/19/2010CA2389525C Variable cycle propulsion device employing exhaust bypass for supersonic aircraft, and operating process
10/14/2010WO2009133273A8 Device with secondary jets reducing the noise generated by an aircraft jet engine
10/14/2010US20100257865 Jet engine nozzle exit configurations and associated systems and methods
10/13/2010EP2239449A2 Nacelle assembly for turbofan aircraft engines
10/13/2010EP2239428A2 Exhaust plenum for a turbine engine
10/13/2010CN101858277A Nacelle assembly for turbofan aircraft engines
10/12/2010US7810335 Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft
10/07/2010WO2010114604A1 Jet nozzle plug with varying non-circular cross sections
10/07/2010WO2009133271A3 Device for reducing noise generated by an aircraft jet engine with curve ducts
10/07/2010US20100251724 Aircraft jet engine provided with a device for reducing propulsion jet noise
10/06/2010CN101253095B Dynamically self-locking catching device
10/05/2010US7805924 Thermally decoupled mixer
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